N410CW
Registered owner: WARANOWITZ GEORGE A, NC (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
5 reports on file, 2006-06-18 – 2006-12-05.
Part: HYDRAULIC SYSTEM — LOW PRESSURE
ON LANDING, CREW REPORTED LOSS OF HYDRAULIC PRESSURE AND NORMAL BRAKES. EMERGENCY BRAKING WAS USED. MAINTENANCE FOUND THE LOW PRESSURE LINE RUPTURED AND LEAKING HYDRAULIC FLUID ON THE LEFT THRUST REVERSER . THE RUPTURE OCCURED APPROXIMATELY 6" FROM THE 90 DEGREE ELBOW FITTING. THERE DID NOT APPEAR TO BE ANY CHAFFING ON THE LINE IN THE AREA WHERE THE RUPTURE OCCURRED. THE LINE WAS REPLACED.
Part: THRUST REVERSER — BROKEN (RIGHT ENGINE) · airframe 4,870 hrs · 4,130 cycles
THE CREW REPORTED THAT AFTER LANDING THE RIGHT THRUST REVERSER DID NOT DEPLOY. BOTH ARM AND UNLOCK LIGHTS ILLUMINATED BUT THE DEPLOY LIGHT DID NOT. DURING THE POST FLIGHT INSPECTION A BROKEN THRUST REVERSER DRIVER ARM WAS FOUND AND THE FAIRING WAS BUCKLED. MAINTENANCE REPLACED THE THRUST REVERSER ASSEMBLY AND PERFORMED INSTALLATION AND FUNCTIONAL CHECKS OF THE SYSTEM WITH NO NOTED DEFECTS. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: ENGINE — LEAKING (RIGHT) · airframe 4,834 hrs · 4,099 cycles
KSFB - KHPN THE CREW REPORTED A SMELL OF BURNING OIL OR A BLEED AIR ODOR FILLED THE COCKPIT AND CABIN ON TAKEOFF. THE ODOR CONTINUED DURING ALL POWER CHANGES AND WHILE VARIOUS POSITIONS OF THE ENVIRONMENTAL CONTROL SYSTEM WERE SELECTED. THE AIRCRAFT WAS DIVERTED TO KPBI FOR MAINTENANCE. MAINTENANCE REPLACED THE RIGHT ENGINE ASSEMBLY DUE TO AN INTERNAL OIL LEAK. THE AIR CYCLE MACHINE COALESCER SOCK WAS REPLACED DUE TO BEING OIL SOAKED. NO DEFECTS WERE NOTED DURING GROUND ENGINE RUNS AT VARIOUS POWER SETTINGS. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: VALVE — DEFECTIVE (AFT FUSELAGE) · airframe 4,831 hrs · 4,095 cycles
ON T/O CREW NOTED A BURNING BLEED AIR ODOR UNTIL AIRCRAFT WAS LEVELED 23,000 FT. IN DESCENT SAME SMELL WAS PRESENT. INSPECTED BLEED AIR COMPONENTS, DISCOVERED CONNECTOR FOR FLOW INCREASING VALVE NOT HOOKED UP. CONNECTOR INSTALLED. NO DISCREPANCIES DURING GROUND OPS CHECKS. RETURNED TO SERVICE. ON 6-22-06 CREW NOTED A BURNING BLEED AIR SMELL UP UNTIL LEVELED OFF, SAME ODOR ON DESCENT. A DEFECTIVE EMERGENCY PRESSURIZATION VALVE DISCOVERED BY MAINTENANCE DURING TROUBLESHOOTING PROCEDURES. PRESSURIZATION VALVE AND ASSOCIATED GASKETS WERE REPLACED. OPERATIONAL CHECKS WERE GOOD DURING OPERATIONAL AND LEAK CHECKS WHILE PERFORMING GROUND ENGINE RUNS. AIRCRAFT WAS RETURNED TO SERVICE.
Part: COALESCER BAG — DIRTY · airframe 4,829 hrs · 4,094 cycles
THE CREW REPORTED THAT A BURNING BLEED AIR SMELL WAS COMING INTO THE COCKPIT ON TAKEOFF BUT HAD DISSIPATED ENTIRELY AFTER ROTATION. BOTH COCKPIT AND CABIN HEAT WAS SET AT FULL COLD. MAINTENANCE CLEANED THE WATER SEPARATOR SOCK. SYSTEM OPERATIONAL CHECKS WERE NORMAL, AND THE AIRCRAFT WAS RETURNED TO SERVICE.